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PROPELLER SHAFT END - FLANGED 4.250(107.95) BOLT CIRCLE
- Aerospace Standard
- AS880
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Rationale
AS880 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
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1
DATUM A IS ROTATIONAL AXIS OF SHAFT: I. E., THE COMMON AXIS OF THOSE SHAFT FEATURES ON WHICH THE SHAFT MOUNTS AND ROTATES: E. G., SPLINES, JOURNALS, ETC.
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2
BREAK EDGES . 003–. 015(0. 08 – 0. 38) UNLESS OTHERWISE SPECIFIED.
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3
SURFACE TEXTURE: ANSI B46.1-1962. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES (3.2 MICROMETRES).
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4
DIMENSIONS IN INCHES(MILLIMETRES). METRIC CONVERSIONS ARE INTERNATIONAL SYSTEM UNITS (SI).
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5
DIMENSIONING AND TOLERANCING: ANSI Y14. 5-1966. ∅ = DIAMETER.
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6
FORM TOLERANCES AND THEIR RELATED DATUMS ARE RFS UNLESS OTHERWISE SPECIFIED.
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7
THIS AEROSPACE STANDARD SUPERSEDES AND CANCELS ARP 880.
THIS IS A DESIGN STANDARD. NOT TO BE USED AS A PART NUMBER.
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Data Sets - Support Documents
No Datasets Available
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
Reference
| Number | Title |
|---|---|
| ANSI/B46.1 | This document is not part of the subscrption. |
| ANSI/Y14.5 | This document is not part of the subscrption. |
| MS9390 | This document is not part of the subscrption. |
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